CN103912318A - Bypass valve assembly of gas machine turbosuperchager - Google Patents

Bypass valve assembly of gas machine turbosuperchager Download PDF

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Publication number
CN103912318A
CN103912318A CN201310006859.9A CN201310006859A CN103912318A CN 103912318 A CN103912318 A CN 103912318A CN 201310006859 A CN201310006859 A CN 201310006859A CN 103912318 A CN103912318 A CN 103912318A
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CN
China
Prior art keywords
rocking arm
gas machine
bypath valve
bypass valve
door assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201310006859.9A
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Chinese (zh)
Inventor
叶双超
张振平
陈超明
谢春琼
陆怡天
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangxi Yuchai Machinery Co Ltd
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Guangxi Yuchai Machinery Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Guangxi Yuchai Machinery Co Ltd filed Critical Guangxi Yuchai Machinery Co Ltd
Priority to CN201310006859.9A priority Critical patent/CN103912318A/en
Publication of CN103912318A publication Critical patent/CN103912318A/en
Pending legal-status Critical Current

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Supercharger (AREA)

Abstract

The invention discloses a bypass valve assembly of a gas machine turbosuperchager. The bypass valve assembly of the gas machine turbosuperchager comprises a rivet, a rocker arm and a bypass valve, wherein the rocker arm is connected to the top face of the bypass valve through the rivet. A rocker arm limiting protrusion is arranged on the top face of the bypass valve. The bypass valve assembly of the gas machine turbosuperchager is simple and reasonable in structure and convenient to install, the radial freedom degree of the bypass valve is limited by arranging the rocker arm limiting protrusion on the top face of the bypass valve, relative rotating abrasion of the bypass valve and the rocker arm is prevented, accordingly untight closing, sticking, dropping and other faults of the bypass valve are avoided, and finally the performance of the turbosuperchager is not influenced.

Description

Gas machine turbocharger bypass door assembly
Technical field
The present invention relates to engine art, particularly a kind of gas machine turbocharger bypass door assembly.
Background technique
Turbosupercharger, because it is to improving engine power, reduce fuel consumption rate, improving effect of discharge aspect, has been widely used in motor.Wherein extensive with the turbosupercharger purposes of exhaust gas by-pass valve, in a large number for diesel engine, petrol engine and gas machine.General turbosupercharger cannot be taken into account low speed and high speed performance, and volute pressurization device low-speed performance less than normal is good, but supercharger impeller easily exceeds the speed limit when high speed, so fall a part of exhaust energy by bypass valve bypass, reduces wheel speed and prevents hypervelocity.Vehicular engine major part all adopts band bypass valve pressurized machine at present.
As depicted in figs. 1 and 2, bypath valve 3 adopts stainless steel to be stamped to form to existing turbocharger bypass door assembly, and rocking arm 2 adopts stamping forming blank to process, and both form by rivet 1 riveted joint again.After riveted joint, bypath valve 3 can rotate freely with respect to the mounting hole of rocking arm 2 together with rivet 1.The applying working condition of diesel engine is generally below rated engine speed, and turbocharger bypass door major part is in closed condition, and now valve does not rotate, and this entirety of valve and rivet is with rocking arm without relative movement, and valve wearing and tearing are few; And the front-seat temperature in diesel engine whirlpool is generally no more than 680 DEG C, so the applying working condition of bypath valve is not severe, on market, the wear-out failure of diesel pressure booster valve is also fewer.
But for gas machine, particularly public transport gas machine, in order to pursue low-speed big and low speed response performance, plateau applicable performance, general institute joins turbosupercharger and is partial to less volute pressurization device, engine speed corresponding when its bypath valve unlatching is lower, and public transport with gas machine frequently start to walk, low speed accelerates, so all frequent switching states in Open-closure of the most of operating mode of turbocharger bypass door.Before gas machine whirlpool, temperature reaches as high as 760 DEG C in addition, so the turbocharger bypass valve of gas machine is badly more many than the working environment of diesel engine.Therefore for gas machine, when bypath valve 3 is opened, under the impact of hot air flow, bypath valve 3 can rotate freely with respect to the mounting hole of rocking arm 2 together with rivet 1, the general opening time of its bypath valve is long, Open-closure switches frequently, the front-seat temperature in whirlpool is higher, and bypath valve wear-out failure is more.
Summary of the invention
The present invention is in order to overcome defect in above-mentioned prior art, provide a kind of simple and reasonable, easy for installation, by the radially degrees of freedom of restriction bypath valve, prevent that bypath valve and rocking arm from relative rotation wearing and tearing, resistant to elevated temperatures gas machine turbocharger bypass door assembly occurring.
For achieving the above object, according to the invention provides a kind of gas machine turbocharger bypass door assembly, comprising: rivet, rocking arm and bypath valve, rocking arm by rivet at bypath valve end face; Bypath valve end face is provided with rocking arm spacing preiection.
In technique scheme, rocking arm spacing preiection is two, is symmetrically distributed in the both sides, end of rocking arm.
In technique scheme, the both sides, end of rocking arm have respectively the semilune boss of an outwardly convex, and the inner side symmetry of rocking arm spacing preiection offers the semilune groove with the adaptive clamping of semilune boss.
In technique scheme, rocking arm spacing preiection is of end sides who is distributed in rocking arm.
In technique scheme, bypath valve is that stainless steel is stamped to form or High Nickel Steel casting forms.
Compared with prior art, the present invention has following beneficial effect: this gas machine turbocharger bypass door assembly is simple and reasonable, easy for installation, by rocking arm spacing preiection being set at bypath valve end face, with the radially degrees of freedom of restriction bypath valve, prevent that bypath valve and rocking arm from relative rotation wearing and tearing occurring, and cause bypath valve to fit badly, stuck, the fault such as come off, the final turbocharger performance that affects, and bypath valve is that stainless steel is stamped to form or High Nickel Steel precision casting forms, high temperature resistant, further improve turbocharger performance.
Brief description of the drawings
Fig. 1 is the plan structure schematic diagram of existing gas machine turbocharger bypass door assembly;
Fig. 2 is the A-A direction sectional structure schematic diagram of Fig. 1;
Fig. 3 is gas machine turbocharger bypass door assembly embodiment's one of the present invention plan structure schematic diagram;
Fig. 4 is the B-B direction sectional structure schematic diagram of Fig. 3;
Fig. 5 is the plan structure schematic diagram of gas machine turbocharger bypass door assembly embodiment's one of the present invention rocking arm;
Fig. 6 is the side-looking structural representation of gas machine turbocharger bypass door assembly embodiment's one of the present invention rocking arm;
Fig. 7 is the structural representation of gas machine turbocharger bypass door assembly embodiment's one of the present invention bypath valve;
Fig. 8 is the C-C direction sectional structure schematic diagram of Fig. 7;
Fig. 9 is gas machine turbocharger bypass door assembly embodiment's two of the present invention plan structure schematic diagram;
Figure 10 is gas machine turbocharger bypass door assembly embodiment's three of the present invention plan structure schematic diagram;
Figure 11 is gas machine turbocharger bypass door assembly embodiment's four of the present invention plan structure schematic diagram.
Embodiment
Below in conjunction with accompanying drawing, a specific embodiment of the present invention is described in detail, but is to be understood that protection scope of the present invention is not subject to the restriction of embodiment.It will be appreciated that, mentioned in following mode of execution of the present invention " on ", D score, " left side ", " right side ", " front " and " reverse side " be all taking the direction shown in each figure as benchmark, these words that are used for limiting direction are only used to be convenient to explanation, do not represent the restriction to the concrete technological scheme of the present invention.
Gas machine turbocharger bypass door assembly of the present invention, by the radially degrees of freedom of restriction bypath valve, prevents that bypath valve and rocking arm from relative rotation wearing and tearing occurring, and then affects turbocharger performance.
Embodiment one:
As shown in Figure 3 and Figure 4, the concrete structure of this gas machine turbocharger bypass door assembly comprises: rivet, Rocker arm 4 and bypath valve 5, and together with Rocker arm 4 passes through rivet with bypath valve 5.
Wherein, as shown in Figure 5 and Figure 6, the end of Rocker arm 4 and bypath valve 5 riveteds is stamped into flat, is convenient to bottom surface, end and novel bypath valve 5 end faces are adjacent to installation; This end offers the rocking arm mounting hole 41 that vertically runs through upper and lower surface, and 42, two semilune boss 42 of semilune boss that the left and right sides has respectively an outwardly convex are symmetrical set.
As shown in Figure 7 and Figure 8, bypath valve 5 is stamped to form or High Nickel Steel precision casting forms for stainless steel, high temperature resistant more than 850 DEG C.What the center of bypath valve 5 was corresponding with rocking arm mounting hole 41 offers the bypath valve center hole 51 that vertically runs through upper and lower surface, the inner side symmetry that the left and right sides of the bypath valve center hole 51 of bypath valve 5 end faces is symmetrically arranged with 52, two spacing preiections 52 of two spacing preiections offers the semilune groove 53 with the 42 adaptive clampings of semilune boss.
When assembling, rivet is through the rocking arm mounting hole 41 of Rocker arm 4 and the bypath valve center hole 51 of bypath valve 5, and be riveted together Rocker arm 4 and bypath valve 5 (the middle mounting zone that the mounting end of Rocker arm 4 is positioned at two spacing preiections 52 of bypath valve 5 end faces).Now, rivet and rocking arm mounting hole 41 are Spielpassung, make bypath valve 5 slightly have certain shifting amount, are convenient to cover tightly the by-pass port on supercharger volute, and prevent that bypath valve 5 is stuck.Two semilune boss 42 respectively clamping enter the semilune groove 53 of two spacing preiections 52, with restriction bypath valve 5 and Rocker arm 4 in degrees of freedom radially, prevent the wearing and tearing of both relative rotary motion, cause that bypath valve fits badly, stuck, the fault such as come off, finally affect turbocharger performance.
Embodiment two:
As shown in Figure 9, rocking arm 6 and bypath valve 7 be by together with rivet, and itself and embodiment's one difference is, the end of rocking arm 6 is stamped into flattened rectangular, and the left and right sides does not have the semilune boss of an outwardly convex.And the left and right sides of the bypath valve center hole of corresponding bypath valve 7 end faces is symmetrically arranged with two spacing preiections 71, the inner side of two spacing preiections 71 does not offer semilune groove yet, two outside butts of the inner side of two spacing preiections 71 and rocking arm 6 ends are spacing, with restriction bypath valve 7 and rocking arm 6 in degrees of freedom radially, prevent both relative rotary motion wearing and tearing, cause that bypath valve fits badly, stuck, the fault such as come off, finally affect turbocharger performance.
Embodiment three:
As shown in figure 10; rocking arm 8 and bypath valve 9 is by together with rivet; it is with embodiment two difference; the right side of the bypath valve center hole of bypath valve 9 end faces is provided with separately a spacing preiection 91; inner side of spacing preiection 91 does not offer semilune groove yet; the right outside side butt of the inner side of spacing preiection 91 and rocking arm 8 ends is spacing; to limit bypath valve 9 and rocking arm 8 in degrees of freedom radially; prevent that both relative rotary motion from wearing and tearing; cause that bypath valve fits badly, stuck, the fault such as come off, finally affect turbocharger performance.
Embodiment four:
As shown in figure 11; rocking arm 8 and bypath valve 9 is by together with rivet; it is with embodiment two difference; the left side of the bypath valve center hole of bypath valve 9 end faces is provided with separately a spacing preiection 91; inner side of spacing preiection 91 does not offer semilune groove yet; the left-external side butt of the inner side of spacing preiection 91 and rocking arm 8 ends is spacing; to limit bypath valve 9 and rocking arm 8 in degrees of freedom radially; prevent that both relative rotary motion from wearing and tearing; cause that bypath valve fits badly, stuck, the fault such as come off, finally affect turbocharger performance.
This gas machine turbocharger bypass door assembly is simple and reasonable, easy for installation, by rocking arm spacing preiection being set at bypath valve end face, with the radially degrees of freedom of restriction bypath valve, prevent that bypath valve and rocking arm from relative rotation occurring and wear and tear, and cause bypath valve to fit badly, stuck, the fault such as come off, the final turbocharger performance that affects, and bypath valve is that stainless steel is stamped to form or High Nickel Steel precision casting forms, high temperature resistant, has further improved turbocharger performance.
Disclosed is above only several specific embodiment of the present invention, and still, the present invention is not limited thereto, and the changes that any person skilled in the art can think of all should fall into protection scope of the present invention.

Claims (5)

1. a gas machine turbocharger bypass door assembly, is characterized in that, comprising: rivet, rocking arm and bypath valve, and described rocking arm passes through described rivet at described bypath valve end face; Described bypath valve end face is provided with rocking arm spacing preiection.
2. gas machine turbocharger bypass door assembly according to claim 1, is characterized in that: described rocking arm spacing preiection is two, is symmetrically distributed in the both sides, end of described rocking arm.
3. gas machine turbocharger bypass door assembly according to claim 2, it is characterized in that: the both sides, end of described rocking arm have respectively the semilune boss of an outwardly convex, the inner side symmetry of described rocking arm spacing preiection offers the semilune groove with the adaptive clamping of described semilune boss.
4. gas machine turbocharger bypass door assembly according to claim 1, is characterized in that: described rocking arm spacing preiection is of end sides who is distributed in described rocking arm.
5. according to the gas machine turbocharger bypass door assembly described in any one in claim 1 to 4, it is characterized in that: described bypath valve is that stainless steel is stamped to form or High Nickel Steel casting forms.
CN201310006859.9A 2013-01-09 2013-01-09 Bypass valve assembly of gas machine turbosuperchager Pending CN103912318A (en)

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Application Number Priority Date Filing Date Title
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160341110A1 (en) * 2013-12-26 2016-11-24 Toyota Jidosha Kabushiki Kaisha Turbocharger with improved bypas valve sealing
CN106285919A (en) * 2015-05-22 2017-01-04 广州汽车集团股份有限公司 Exhaust gas bypass device and there is its turbocharger
CN106523137A (en) * 2016-12-05 2017-03-22 无锡康明斯涡轮增压技术有限公司 Bypass valve with anti-rotation structure
US10578216B2 (en) 2014-09-12 2020-03-03 Denso Corporation Valve device
CN112912600A (en) * 2018-09-12 2021-06-04 马勒金属制品有限公司 Safety valve for turbocharger and method of manufacturing the same
DE102021210637A1 (en) 2021-09-23 2023-03-23 Vitesco Technologies GmbH Valve flap device for a wastegate valve of an exhaust gas turbocharger and exhaust gas turbocharger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007064551A1 (en) * 2005-11-29 2007-06-07 Honeywell International Inc. Non-rotating turbocharger waster gate valve
DE202010005747U1 (en) * 2010-04-19 2010-07-29 Zollern Gmbh & Co. Kg Valve flap for a blow-off valve of a turbocharger
US20120234002A1 (en) * 2011-03-14 2012-09-20 Honeywell International Inc. Wastegates and Wastegate Components
DE102011075201A1 (en) * 2011-05-04 2012-11-08 Bosch Mahle Turbo Systems Gmbh & Co. Kg Charging device, particularly exhaust gas turbocharger, for internal combustion engine, particularly of motor vehicle, has damping element that is arranged in or at drive train, particularly between spindle and bush
CN203097958U (en) * 2013-01-09 2013-07-31 广西玉柴机器股份有限公司 Gas machine turbocharger by-pass valve assembly

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007064551A1 (en) * 2005-11-29 2007-06-07 Honeywell International Inc. Non-rotating turbocharger waster gate valve
DE202010005747U1 (en) * 2010-04-19 2010-07-29 Zollern Gmbh & Co. Kg Valve flap for a blow-off valve of a turbocharger
US20120234002A1 (en) * 2011-03-14 2012-09-20 Honeywell International Inc. Wastegates and Wastegate Components
DE102011075201A1 (en) * 2011-05-04 2012-11-08 Bosch Mahle Turbo Systems Gmbh & Co. Kg Charging device, particularly exhaust gas turbocharger, for internal combustion engine, particularly of motor vehicle, has damping element that is arranged in or at drive train, particularly between spindle and bush
CN203097958U (en) * 2013-01-09 2013-07-31 广西玉柴机器股份有限公司 Gas machine turbocharger by-pass valve assembly

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160341110A1 (en) * 2013-12-26 2016-11-24 Toyota Jidosha Kabushiki Kaisha Turbocharger with improved bypas valve sealing
US10082071B2 (en) * 2013-12-26 2018-09-25 Toyota Jidosha Kabushiki Kaisha Turbocharger with improved bypass valve sealing having a positioning bolt
US10578216B2 (en) 2014-09-12 2020-03-03 Denso Corporation Valve device
CN106285919A (en) * 2015-05-22 2017-01-04 广州汽车集团股份有限公司 Exhaust gas bypass device and there is its turbocharger
CN106285919B (en) * 2015-05-22 2019-05-03 广州汽车集团股份有限公司 Exhaust gas bypass device and turbocharger with it
CN106523137A (en) * 2016-12-05 2017-03-22 无锡康明斯涡轮增压技术有限公司 Bypass valve with anti-rotation structure
CN112912600A (en) * 2018-09-12 2021-06-04 马勒金属制品有限公司 Safety valve for turbocharger and method of manufacturing the same
DE102021210637A1 (en) 2021-09-23 2023-03-23 Vitesco Technologies GmbH Valve flap device for a wastegate valve of an exhaust gas turbocharger and exhaust gas turbocharger

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Application publication date: 20140709